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ENGINES LINER SHIELDS COVERS AND DUCTS Parts 6037T92G03 through 6886426

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We solve sourcing challenges for parts like 6037T92G03, 4047947, 4047947, 614304, B928809, 706550-5, 723869-5, 4038948, 4038948, 4047868 -- hard to find, long lead time, and obsolete part requirements.

Part number	Description	Category	Details
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6037T92G03	LINER, COMBUSTION	III END ITEM IDENTIFICATION	ENGINE MODEL TF34
4047947	SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE	MATERIAL	NICKEL ALLOY SHIELD
4047947	SHIELD, HEAT, AIRCRAFT GAS TURBINE ENGINE	MATERIAL	NICKEL ALLOY SHIELD
614304	BRACE, INLET CASE	GENERAL CHARACTERISTICS ITEM DESCRIPTION	TITANIUM PER AMS 4921,1.985 IN. OD,1.148 IN. ID,0.390 IN. THK O/A
B928809	CASING ASSEMBLY
706550-5	CAP, EXHAUST DUCT	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,AMS 5596,O/A DIM. 0.056 IN. MIN. THICKNESS,0.064 IN. MAX. THICKNESS,14.680 IN. L
723869-5	CAP, EXHAUST DUCT	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,AMS 5596,O/A DIM. 0.056 IN. MIN. THICKNESS,0.064 IN. MAX. THICKNESS,14.680 IN. L
4038948	PLATE, AUGMENTOR COMBUSTION CHAMBER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,CORROSION RESISITANT,AMS 5596,ROCKWELL HARDNESS C,O/A DIM. 1.830 IN. L,0.641 IN. W,0.027 IN. MIN. THICKNESS,0.031 IN. MAX. THICKNESS
4038948	PLATE, AUGMENTOR COMBUSTION CHAMBER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,CORROSION RESISITANT,AMS 5596,ROCKWELL HARDNESS C,O/A DIM. 1.830 IN. L,0.641 IN. W,0.027 IN. MIN. THICKNESS,0.031 IN. MAX. THICKNESS
4047868	STIFFENER, COMBUSTION CHAMBER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	COBALT ALLOY
4047867	STIFFENER, COMBUSTION CHAMBER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,CORROSION RESISTANT,AMS 5599
4047866	STIFFENER, COMBUSTION CHAMBER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	STEEL,CORROSION RESISTANT,AMS 5599
4047851	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	CRITICALITY CODE JUSTIFICATION	AGAV
4047864	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	CRITICALITY CODE JUSTIFICATION	AGAV
23058707	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	MATERIAL	STEEL CORROSION RESISTING OVERALL
23058707	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	MATERIAL	STEEL CORROSION RESISTING OVERALL
6876863	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	MATERIAL	STEEL CORROSION RESISTING OVERALL
6894068	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	MATERIAL	STEEL CORROSION RESISTING OVERALL
6894068	LINER, COMBUSTION CHAMBER, AIRCRAFT GAS TURBINE ENGI	MATERIAL	STEEL CORROSION RESISTING OVERALL
7032M42G01	LINER, EXHAUST DUCT, AIRCRAFT GAS TURBINE ENGINE	MATERIAL	STEEL OVERALL
4047T87P01	COWL, OUTER COMBUSTION LINER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	CRES AMS5599,16.895 IN. MIN OD,16.995 IN. MAX OD,14.941 IN. MIN ID,14.971 IN. MAX ID,1.160 IN. MIN H,1.200 IN. MAX H
4047T87P01	COWL, OUTER COMBUSTION LINER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	CRES AMS5599,16.895 IN. MIN OD,16.995 IN. MAX OD,14.941 IN. MIN ID,14.971 IN. MAX ID,1.160 IN. MIN H,1.200 IN. MAX H
4047T87P01	COWL, OUTER COMBUSTION LINER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	CRES AMS5599,16.895 IN. MIN OD,16.995 IN. MAX OD,14.941 IN. MIN ID,14.971 IN. MAX ID,1.160 IN. MIN H,1.200 IN. MAX H
4048T33P01	COWL, INNER COMBUSTION LINER	GENERAL CHARACTERISTICS ITEM DESCRIPTION	CRES AMS5599,12.860 IN. MIN OD,12.890 IN. MAX OD,12.110 IN. MIN ID,12.140 IN. MAX ID,1.620 IN. MIN H,1.660 IN. MAX H
6886426	DIAPHRAGM ASSY, CASE	CRITICALITY CODE JUSTIFICATION	AGAV